Helicopter Maneuvers and Angular Momentum

Aug 30, 2024

Lecture Notes: Conservation of Angular Momentum in Helicopters

Introduction

  • Speaker: Jacob
  • Topic: Conservation of Angular Momentum and its application in helicopter maneuvering flight.
  • Context: Effects typically experienced during aggressive helicopter maneuvers, not in standard flight patterns.

Conservation of Angular Momentum

  • Definition: Angular momentum of a rotating body remains constant unless acted upon by external forces.
  • Relation to Newton's Law: Variation applied to rotating bodies.
  • Application to Helicopters: Rotor blades try to conserve their angular momentum.

Coriolis Effect

  • Definition: Tendency of a rotating body to increase velocity as its center of gravity moves closer to the axis of rotation.
  • Relation to Angular Momentum: Used interchangeably in this lecture.

Helicopter Flight Mechanics

  • Maneuvering Flight Effects:
    • Increased G loading affects rotor system.
    • Rotor begins to cone (increasing coning angle).
    • Blade diameter shrinks as coning occurs.
    • Center of gravity shifts closer to the axis of rotation.
    • Rotor RPM changes as a result.

Comparison Examples

  • Figure Skater Analogy:
    • Arms closer = increased RPM.
    • Arms extended = decreased RPM.
  • Racecar on Track:
    • Shorter track loop = more revolutions per minute while maintaining the same speed.

Engine Control System in Helicopters

  • Function: Maintains rotor RPM.
  • Response to RPM Changes:
    • Decrease fuel flow when rotor RPM increases.
    • Increase fuel flow when rotor RPM decreases.

Potential Issues and Considerations

  • Rapid Rotor Fluctuations:
    • Can lead to overspeeding or underspeeding of rotors.
    • Possible over-torqueing if engine fuel adjustments aren’t timely.
  • Pilot Considerations:
    • Awareness of rotor RPM and torque fluctuations is crucial.
    • Anticipate changes with collective application to avoid exceeding limits.

Conclusion

  • Key Takeaway: Rotor blades aim to maintain momentum; G loading causes RPM changes.
  • Impacts on Aircraft: Potential for over-speed, under-speed, or over-torque conditions.
  • Pilot Advice: Understanding rotor RPM changes is critical for safe maneuvering.

Closing

  • Reminder: Understanding rotor dynamics is essential for flight safety.
  • Call to Action: Like and subscribe for more helicopter lessons.
  • Presented by: Jacob, "Helicopter Lessons in Ten Minutes"